375
Table1.
_______________________________________________
Length[m]277.5 11.56
Breadth[m]43.2 1.80
Draft[m]12.0 0.50
BlockcoefficientC
B[‐]0.79 0.79
Scale‐1:24
Numberofazipods 2 2
_______________________________________________
The configuration of the stern part of the ship
modelispresentedinfigureno4.Youcanclearlysee
the specific shape of the stern of the ship equipped
with azipod propulsion improving the propulsion
effectivenessand significant skeg area enhancing
thecoursestability.
Figure4.TheLNGcarriermodelequippedwithtwo pulling
azipods used for stopping tests (in this photo the pulling
azipodsareturnedaroundby180degrees)
The model tests were carried out on the lake in
deepwater.Thewindvelocityduringtestswasabout
5 knots and less (after conversion to the real ship
scale).Currentwasnotobserved.
Tests were performed with an initial speed of
about12knots,thatis,forthespeedof
approx.65%of
theservicespeedofatypicallargeLNGcarrier.This
speed does not coincide with recommendations in
standards of manoeuvrability [4], where 90% of the
servicespeedissuggested. Suchachoicewasdictated
howeverbythedemandsofthetraining.
Propellerrevolutionsworkingbackwerethe
same
asintheforwardmotion.Theinstantaneousposition
of azipods and number of revolutions of installed
propellers was also measured. The position of
azipods and number of their revolutions were
changed manually by operators performing
experiment.
The model trajectory, heading and speed were
measuredusingpreciseGPSsystemoperatingin
RTK
mode.
a/. b/.
Figure 5 Comparison of outward (a) and inward (b)
directionofazipodturning
The azipod slew velocity was 7.5 º/s, time for
reversingdirectionofpropellerrevolutionswas 60 s
(bothparametersgivenfortherealship).
Thefollowingstoppingtrialswereperformed:
1 Inertia stopping (propellers windmilling)with the
azipodangleofdeflection90ºoutwards;
2 Stopping with the azipod angle of deflection 90º
outwards.Propellersrevolutionsnotchanged.
3 Stopping with the azipod angle of deflection 90º
inwards.Propellersrevolutionsnotchanged.
4 Stoppingbyturningazipodsaround(180°).When
turningnumberofpropellersrevolutionsreduced,
afterwardspropellerrevolutionsreturnedback..
5 Stopping by changing the propellers direction of
revolution.Asternnumber
ofpropellerrevolutions
thesameasahead.
6 Stopping by indirect manoeuvre: deflection of
azipods 30º outwards, afterwards changing the
propellersdirectionofrevolution.
4 EXPERIMENTALDATA
Resultsofmodeltestsarepresentedintable2below.
The stopping distance is given in non‐dimensional
form as the ratio of track
reach to the shipʹs length
S
d/L (track reach is the total distance travelled along
the ship's path):
Table2.
_______________________________________________
Case DescriptionofthestoppingprocedureSd/L
_______________________________________________
1 Inertiastopping(propellerswindmilling)with 11.2
theazipodsangleofdeflection90ºoutwards
2 Stoppingwiththeazipodsangleofdeflection90º 4.0
outwards.Propellersrevolutionsnotchanged.
3 Stoppingwiththeazipodsangleofdeflection90º 3.8
inwards.Propellersrevolutionsnotchanged.
4 Stoppingbyturningazipods
around(180°).When 2.7
turningazipods,numberofpropellersrevolutions
reduced,afterwardspropellerrevolutionsreturned
back.
5 Stoppingbychangingthepropellersdirectionof 4.4
revolution.Asternnumberofpropeller
revolutionsthesameasahead.
6 Stoppingbyindirectmanoeuvre:deflectionof 3.7
azipodsby30ºoutwards,
withsimultaneous
reversingofpropellers.Asternnumberof
propellersrevolutionsthesameasahead
_______________________________________________
Some recorded trajectories of the model are also
shown.Arepresentedsuccessivelytrajectoriesforthe
followingstoppingmanoeuvres:
Inertiastopping(propellerswindmilling)withthe
azipodsangleofdeflection90ºoutwards
(case described as number 1 in the table no 2,
trajectoryshowninfig.6a)
Stopping by changing the propellers direction of
revolutions (case described as number 5in the
tableno2,trajectoryshowninfig.6b)
Stopping by turning azipods around (case
described as number 4in the table no 2,
trajectoryshowninfig.6c)